Simple, Versatile and Cost Effective
Hybrid Rocket propulsion systems
Simple, Versatile and Cost Effective Hybrid Rocket propulsion systems to provide mobility to satellite platforms and large deployers in a range between 100 N to 10 kN of thrust.
The system is specifically conceived to represent a trade off between costs and performances, targeting a substantial cost reduction respect to currently available, MMH-N2O4 bi-propellant units.
The system is customizable on thrust, expansion ratio and accommodation to fit specific customer needs.
Hydrogen peroxide is a green non toxic oxidizer. Furthermore our system uses highly stabilized peroxide which, respect to MIL-Grade peroxide allows for reduced compatibility issues. Different type of solid fuels can be used depending on customer needs, all of them are not reactive and not toxic.
The system is restartable many times.
The system allows for a 12:1 throttleability.
Current delivered specific impulse 285 s.
Orbit raising, Orbit changes, Decommissioning, KO motor.
Different versions of the motor are under development since 2014. Several laboratory models have been developed and tested. A 500 N Engineering model is under development. Currently TRL 5/6.
Developments are currently ongoing to target TRL 6.